N661HA, cancelled Jul 20, 2005
Service difficulty reports · 47
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N661HA' AND deregistration_id = 'N661HA-2005-07-20' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N661HA' AND deregistration_id = 'N661HA-2005-07-20' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR HALA0100056Gcu · failedFLT 184 - HNL - AIRCRAFT X-TIE LOCKOUT LIGHT CAME ON IN FLIGHT. IT CAUSED A DOUBLE GENERATOR FAILURE, RESET GENERATORS IN FILGHT. APU WAS RESTARTED SUCCESSFULLY. NORMAL LANDING. REPLACED RIGHT GCU. GROUND RAN BOTH ENGINES. OPS CHECK OK. RESET X-TIE LOCKSDR HALA0000240Acm · failedOGG - FLT 112 - SMOKE AND VERY STRONG BURNING SMELL IN CABIN WITH NR 1 LEFT AC PACK ON. OK TO CONTINUE PER MEL 21-1 DMI NR 13681 TRANSCRIBED TO HAL M443 AND MPCW CAT C. REMOVED AND REPLACED NR 1 ACM PER MM 21-51-1. OPS AND LEAK CHECK GOOD. (M)SDR HALA9900195Cotter Key · out of positionFLT 113 - HNL - ON APPROACH TO LIH, WHEN GEAR HANDLE PLACED DOWN, BOTH MAINS CAME DOWN. NOSE GEAR DID NOT COME DOWN. FOLLOWED SOP. RETURNED HNL. GEAR CAME DOWN 3 GREEN. INSPECTED NOSE GEAR COND AND SECURITY CHECK GOOD WIRING CHECK GOOD. REPLACED L/G PROXSDR HALA9900194Window · crackedMAE - CABIN WINDOW NR 26 LEFT INTERNAL DOUBLER TOP FORWARD EDGE IS CRACKED AT STATION 693 LONGERON 12L. REPAIRED WINDOW RING PAN IAW EA 9-5310-19-A0458 AND SRM 51-30-2. (M)SDR HALA9900193Splice · crackedMAE - FUSELAGE SKIN PRODUCTION SPLICE IS CRACKED JUST BELOW LONGERON 17R BETWEEN FS 1247 AND FS 1258. TRIM OUT OF PRODUCTION SPLICE BETWEEN LONGERON 17R AND 16R AND INSTALLED SPLICE DOUBLER PER EA 9-5333-19-A0455. (M)SDR HALA9900192Panel · corrodedMAE - LEFT WING TE FLAP LOWER SIDE AT PANEL 1523A, SKIN AND RIB ARE CORRODED. REMOVED AND REPLACED RIB, ANGLE, AND SKIN IAW SRM 51-30-2 AND 51-30-5. (M)SDR HALA9900191Longeron · crackedAFT CARGO LONGERON 26L IS CRACKED AT STATION 964. REMOVED AND INSTALLED REPAIR TO LONGERON 26L IAW SRM 51-30-2 AND 51-30-5 AND EA 9-5314-19-A0469. (M)SDR HALA9900190Skin · corrodedMAE - RT WING T/E FLAP INBOARD END OUTER SKIN HAS CORROSION ON ENTIRE AREA AFT OF MOVEABLE VANE. REMOVED SKIN AND DOUBLER AND REPLACED IAW 51-30-2 AND 51-10-4 AND EA 9-5750-19-A0460. (M)SDR HALA9900119Switch · failedHNL - FLT 106 - FLIGHT ATTENDANTS REPORT HAZE AND UNUSUAL ODOR IN CABIN AND SMOKE ALARM ACTIVATION. REPLACED APU OIL PRESSURE SEQUENCE SWITCH, OPS CHECK OK. (M)SDR HALA9800346Battery · dischargedHNL - FLT 106 - EMERGENCY LIGHTS OVERHEAD, INOP ROWS 6-10. REMOVED AND REPLACED BATTERY, OPS CHECK GOOD. (M)SDR HALA980340Battery · dischargedHNL - FLT 102 - (LOG PAGE NR A 154589) - OVERHEAD EMERGENCY LIGHTS ROWS 6-11 INOPERABLE. REPLACED BATTERY, OPS CHECK OK. (X)SDR HALA9800264Battery · dischargedHNL - LOG PAGE NR A143926 - EMERGENCY LIGHTS CEILING BATH ABOVE ROW 10 HAS A WEAK BATTERY. REPLACED BATTERY, OPS CHECK GOOD. (X)SDR HALA9800129Sensor Target · wornHNL - FLT 61 - (LOG PAGE A140341). ON CLIMB-OUT WITH HYDRAULIC PUMP ON HIGH, RT GEAR UNSAFE LIGHT AND GEAR DOOR OPEN LIGHT CAME ON. IT STAYED ON APPROXIMATELY 30 SECONDS THEN WENT OUT. BEFORE ACTION COULD BE TAKEN, GEAR-UP LATCH CHECKED GOOD AFTER LIGHT WENSDR HALA9800123Control Cable · bindingITO - FLT 122 - (LOG PAGE A140193). LEFT ENGINE STUCK IN IDLE. NO RESPONSE FROM THROTTLES. FOUND POWER CABLE ON QUADRANT, ENGINE SIDE BINDING. RE-SECURED POWER CABLE, OPS CHECK OK. RUN-UP CHECK OK. SECURITY CHECK OK. (X)SDR HALA9800071Batteries · dischargedHNL - FLT 512 - EMERGENCY LIGHT CEILING ROW 6-12 DOES NOT COME ON DURING PREFLIGHT TEST. REPLACED BATTERY FOR EMERGENCY LIGHTS FOR ROW 6-12, OPS CHECK OK. (M)SDR HALA9800053Chafe Strips · failedHNL - FLT 177 - LOG PAGE NR A137992 - FLUTTER/VIBRATION AND RUMBLE FELT AT .75 MACH AND ABOVE. (FEELS AERODYNAMICALLY GENERATED). REMOVED AND REPLACED TWO CHAFE STRIPS ON BOTH THE LEFT AND THE RIGHT SPOILERS. (X)SDR HALA9800047Batteries · dischargedHNL - LOG PAGE NR A136850 - CAPTAIN'S OVERHEAD EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED THE BATTERIES AND THE OPERATIONAL CHECK WAS OK. (X)SDR HALA970036Fitting · corrodedDURING C-CHECK INSPECTION, FOUND FITTING P/N 3932805-501 CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED FITTING IAW SRM 53-04 FIG 43 SHEET 3. (M)SDR HALA9700314Longeron · corrodedLONGERON 30 CORRODED BEYOND LIMITS BETWEEN MLG WELLS. FABRICATED AND INSTALLED LONGERON PER SRM 53-04 FIGURE 43. (M)SDR HALA9700313Fitting · corrodedFITTING P/N 3932805-501 CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED FITTING IAW SRM 53-04 FIG 43 SHEET 3. (M)SDR HALA9700310Frame · corrodedFOUND CORROSION AT BASE OF TAILCONE FRAME, APPROX 28 INCHES LEFT AND RIGHT OF 6 O'CLOCK POSITION. REMOVED DAMAGED FRAMES, INSTALLED NEW FRAMES PER SRM 51-30-0 AND DWG 991957. (M)SDR HALA9700309Longeron · corrodedLOWER FUSELAGE CORROSION ON LONGERON 28R FS 733-753. REMOVED DAMAGED SECTION, ACCOMPLISHED SPLICE REPAIR PER SRM 51-30-05 AND 53-02. (M)SDR HALA9700308Longeron · corrodedLONGERON 30 BETWEEN FS 870-889 IS CORRODED. REMOVED DAMAGED SECTION OF LONGERON, FABRICATED AND INSTALLED REPAIR SECTION AND SPLICE PER SRM 53-03 FIG 2A - 7005 CONFIG. (M)SDR HALA9700307Doubler · crackedINTERNAL TITANIUM DOUBLER BETWEEN FS 654 AND 699 LONGERON 25L TO 25R IS CRCKED AT LONGERON 25R. GAINED ACCESS, TRIMMED OUT DAMAGE. VERIFIED DAMAGE CONTAINMENT BY HFEC, FABRICATED AND INSTALLED 7075-T6.071 EXTERNAL DOUBLER AND .025 INCH TITANIUM INTERNAL DOUBSDR HALA9700304Frame · crackedFOUND CRACK IN RADIUS OF FRAME TO SKIN ANGLE, FORWARD OF CAPTAINS WINDSHIELD, APPROX FS 83 BY 9. FABRICATED AND INSTALLED TWO DOUBLERS FROM 7075-T6 .090 INCH PER SRM 53-03 FIG 34. (M)SDR HALA9700303Frame · crackedCRACK IN RADIUS OF FRAME TO SKIN ANGLE, FORWARD OF F/O WINDSHIELD, APPROX FS 83 BY 9.0. STOP DRILLED CRACK, FABRICATED AND INSTALLED TWO ANGLE REPAIR PER SRM 53-03 FIG 34. (M)SDR HALA9700302Trunnion · corrodedRIGHT MLG TRUNNION FITTING HAS CORROSION ON OUTBOARD WING MOUNT FLANGE. REPLACED TRUNNION FITTING AND BUSHED HOLES IN MATING STRUCTURE PER SABRE TECH EA DC9-57-036 TREATED AND PRIMED. (M)SDR HALA9700301Trunnion · corrodedLEFT MLG TRUNNION IS CORRODED. REPLACED TRUNNION, BUSHED HOLES IN MATING STRUCTURE PER SABRE TECH EA DC9-57-040 TREATED AND PRIMED. (M)SDR HALA9700298Stringer · corrodedFOUND CORROSION ON LOWER AFT LEG, STRINGER 11, XCW 58.5 TO XRS 91, RT. REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER STRAPS PER SRM 57-08 METHOD 2. TREATED AND PRIMED. (M)SDR HALA9700252Stringer · corrodedDURING C-CHECK INSPECTION, FOUND CORROSION ON LOWER AFT LEG, STRINGER 11, XCW 58.5 TO XRS 91, RT. REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER STRIPS PER SRM 57-08 METHOD 2, TREATED AND PRIMED. (M)SDR HALA9700251Spar Cap · corrodedDURING C-CHECK INSPECTION, FOUND CORROSION ON FORWARD SPAR LOWER CHORD, XCW 58.5 TO XRS 61.0, LT. REPAIRED BY BLENDOUT, HFEC INSPECTED WITH NO NEGATIVE FINDINGS. RESTORED FINISH, PER SABRE TECH EA DC9-57-042 WITH OEM DER APPROVAL. (M)SDR HALA9700250T-Cap · corrodedDURING C-CHECK INSPECTION, FOUND CORROSION ON T-CAP HORIZONTALLY LEG STATION 58.5 RIGHT FWD TO AFT SPAR. BLENDED OUT DAMAGE, HFEC INSPECTED WITH NO DEFECTS NOTED, RESTORED FINISH, ACTION DER APPROVED PERMANENT REPAIR. (M)SDR HALA9700249Trunnion · corrodedDURING C-CHECK INSPECTION, FOUND LEFT MLG TRUNNION IS CORRODED. REPLACED TRUNNION, BUSHED HOLES IN MATING STRUCTURE PER SABRE TECH EA DC9-57-040, TREATED AND PRIMED. (M)SDR HALA9700248Trunnion · corrodedDURING C-CHECK INSPECTION, FOUND RT MLG TRUNNION FITTING HAS CORROSION ON OUTBOARD WING MOUNT FLANGE. REPLACED TRUNNION FITTING AND BUSHED HOLES IN MATING STRUCTURE PER SABRE TECH EA DC9-57-036, TREATED AND PRIMED. (M)SDR HALA9700247Bulkhead Clip · crackedDURING C-CHECK INSPECTION, FOUND AFT PRESSURE BULKHEAD (RT SIDE) OUT BOARD LOWER CLIP CRACKED AT LONGERON 14. REMOVED DAMAGED MATERIAL, VERIFIED DAMAGE CONTAINMENT BY HFEC, FABRICATED AND INSTALLED AND END CLIPS AND RADIUS BLOCKS PER DAC REPAIR DWG JO60110. SDR HALA9700246Frame · crackedDURING C-CHECK INSPECTION, FOUND CRACK IN RADIUS OF FRAME TO SKIN ANGLE, FWD OF F/O WINDSHIELD, APPROX FS 83 BY 9. STOP DRILLED CRACKED, FABRICATED AND INSTALLED TWO ANGLE REPARI PER SRM 53-03 FIG 34. (M)SDR HALA9700245Frame · crackedDURING C-CHECK INSPECTION, FOUND CRACK IN RADIUS OF FRAME TO SKIN ANGLE, FWD OF CAPTAINS WINDSHIELD, APPROX FS 83 BY 9. FABRICATED AND INSTALLED TWO DOUBLERS FROM 7075-T6 .090 INCH PER SRM 53-03 FIG 34. (M)SDR HALA9700242Doubler · crackedDURING C-CHECK INSPECTION, FOUND INTERNAL TITANIUM DOUBLER BETWEEN FS 654 AND 699 LONGERON 25L TO 25R IS CRACKED AT LONGERON 25R. GAINED ACCESS, TRIMMED OUT DAMAGE, VERIFIED DAMAGE CONTAINMENT BY HFEC. FABRICATED AND INSTALLED 7075-T6.071, EXTERNAL DOUBLER ASDR HALA9700241Longeron · corrodedDURING C-CHECK INSPECTION, FOUND LONGERON 30 BETWEEN FS 870-889 IS CORRODED. REMOVED DAMAGED SECTION OF LONGERON, FABRICATED AND INSTALLED REPAIR SECTION AND SPLICE PER SRM 53-03 FIG 2A, 7005 CONFIG. (M)SDR HALA9700240Longeron · corrodedDURING C-CHECK INSPECTION, FOUND LOWER FUSELAGE, CORROSION ON LONGERON 28R FS 733-753. REMOVED DAMAGED SECTION, ACCOMPLISHED SPLICE REPAIR PER SRM 51-30-05 AND 53-02. (M)SDR HALA9700239Frame · corrodedDURING C-CHECK INSPECTION, FOUND CORROSION AT BASE OF TAIL CONE FRAME, APPROX 28 INCHES LEFT RIGHT OF 6 O'CLOCK POSITION. REMOVED DAMAGED FRAMES, INSTALLED NEW FRAMES PER SRM 51-30-0 AND DWG 991957. (M)SDR HALA9700237Structure · corrodedDURING C-CHECK INSPECTION, FOUND AFT FUSELAGE AREA CORRODED BETWEEN 1260 AND 1292 CANTED FRAMES BETWEEN LONGERONS 10R AND 13R. REMOVED ALL CORROSION AND RESTORED FINISH, FS 1260 L12L CANTED FRAME SUPPORT BAR, LONGERON CAP STIFFENER FS 1260-1275, AND LONGERON SDR HALA9700235Longeron · corrodedDURING C-CHECK INSPECTION, FOUND LONGERON 29R CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED LONGERON. (M)SDR HALA9700234Longeron · corrodedDURING C-CHECK INSPECTION, FOUND LONGERON 30 CORRODED BEYOND LIMITS BETWEEN MLG WELLS. FABRICATED AND INSTALLED LONGERON PER SRM 53-04 FIGURE 43. (M)SDR HALA97126Nlg · bird strikeHNL - DURING LANDING POSSIBLE BIRD STRIKE IN VICINITY OF NOSE AREA UNDERCARRIAGE. CHECKED CONDITION AND SECURITY OF NOSE GEAR AREA. ALSO, CHECKED NR 1 AND NR 2 ENGINE INTAKES. OK FOR SERVICE, NO DEFECTS NOTED. (M)SDR HALA97112Shutoff Valve · failedHNL - FLT 522 - FROM LOG PAGE 122617: ACFT HAS NOTICEABLE WOBBLE ABOVE 290 KNOTS CL/DESCENT/CRUISE WITHOUT AP YAW DAMPER OR RUDDER POWER. DUE TO NOTICEABLE AC WOBBLE ABOVE 290 KNOTS, CL/DESCENT/CRUISE REF LOG PAGE 122617 TEST FLIGHT REQUIRED. REPLACED RUDDESDR HALA9737Bearing · wornHNL - FLT 524 - FROM LOG PAGE 124685: AT AIRSPEEDS GREATER THAN 300 KIAS, THE ACFT HAS A RUMBLE AND WOBBLE THAT IS MORE PRONOUNCED AT WEIGHTS LESS THAN 95,000 POUNDS. RUMBLE/WOBBLE OCCURS WITH OR WITHOUT AUTOPILOT ON. RUDDER SERVO WITH YAW DAMPER ON SHOWS A
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